CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > Siemens > STAR-CCM+

how to form a continuous surface for the derived sections

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   May 7, 2019, 10:21
Default how to form a continuous surface for the derived sections
  #1
New Member
 
Rob
Join Date: May 2019
Posts: 3
Rep Power: 6
Rob715 is on a distinguished road
Hello all,
I want to perform an (m',thera) wrap in star-ccm+, but there are multiple parts in a displayer. I do not know how to form a continuous surface for the multiple sections of derived part.
For example, in the attached picture, the section of rotor region in the front and the section of stator region back, are in the same span. how to form a continuous surface for them? how to perform an (m', theta) wrap?
Any help would be appreciated.
Attached Images
File Type: png ??15.png (13.6 KB, 23 views)
Rob715 is offline   Reply With Quote

Old   May 7, 2019, 11:41
Default
  #2
Senior Member
 
Matt
Join Date: Aug 2014
Posts: 947
Rep Power: 17
fluid23 is on a distinguished road
The way you phrased this question is very confusing. Can you clarify what you are trying to accomplish?
fluid23 is offline   Reply With Quote

Old   May 7, 2019, 12:44
Default
  #3
New Member
 
Rob
Join Date: May 2019
Posts: 3
Rep Power: 6
Rob715 is on a distinguished road
Quote:
Originally Posted by fluid23 View Post
The way you phrased this question is very confusing. Can you clarify what you are trying to accomplish?
thanks for your reply. I am trying to perform Blade-to-blade projection in star-ccm+.
Rob715 is offline   Reply With Quote

Reply


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
Cannot Figure Out How to Transform Part Surface to Derived Part gkhokhar STAR-CCM+ 1 December 2, 2018 21:32
[snappyHexMesh] SnappyHexMesh no layers and no decent mesh for complex geometry pizzaspinate OpenFOAM Meshing & Mesh Conversion 1 February 25, 2015 07:05
Derivation of Momentum Equation in Integral Form Demonwolf Main CFD Forum 2 October 29, 2009 19:53
CFX4.3 -build analysis form Chie Min CFX 5 July 12, 2001 23:19
Wigley form with free surface Renato Main CFD Forum 0 May 10, 2001 17:08


All times are GMT -4. The time now is 20:45.